|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:bore
|
5.5 in
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:cylinderCount
|
5
|
|
gptkbp:displacement
|
9.0 L
549 in³
|
|
gptkbp:drivetrain
|
overhead valve
|
|
gptkbp:emissionsStandard
|
single exhaust
|
|
gptkbp:engine
|
150 lb
military aviation
civil aviation
42 in
front-mounted
36 in
influenced radial engine design
|
|
gptkbp:engineConfiguration
|
5-cylinder radial
|
|
gptkbp:enginePower
|
300 hp at 1,800 rpm
|
|
gptkbp:engineType
|
gptkb:J-5G
J-5A
J-5D
J-5E
J-5F
J-5H
J-5J
J-5K
J-5B
J-5C
|
|
gptkbp:firstRace
|
1925
|
|
gptkbp:fuelType
|
aviation gasoline
magneto
carburetor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright J-5 Whirlwind
|
|
gptkbp:is_used_in
|
gptkb:Wright_Model_B
gptkb:Boeing_40
gptkb:Curtiss_JN-4
gptkb:Wright_Flyer
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notableUsers
|
gptkb:United_States_Navy
gptkb:United_States_Army_Air_Service
|
|
gptkbp:powerOutput
|
300 hp
|
|
gptkbp:productionYears
|
1925-1935
|
|
gptkbp:propulsion
|
fixed-pitch
|
|
gptkbp:setting
|
air-cooled
|
|
gptkbp:stroke
|
6.0 in
|
|
gptkbp:successor
|
gptkb:Wright_R-1300
|
|
gptkbp:torque
|
1,200 lb-ft
|
|
gptkbp:type
|
radial engine
|
|
gptkbp:weight
|
150 lb
|